JPS6320907B2 - - Google Patents
Info
- Publication number
- JPS6320907B2 JPS6320907B2 JP59088361A JP8836184A JPS6320907B2 JP S6320907 B2 JPS6320907 B2 JP S6320907B2 JP 59088361 A JP59088361 A JP 59088361A JP 8836184 A JP8836184 A JP 8836184A JP S6320907 B2 JPS6320907 B2 JP S6320907B2
- Authority
- JP
- Japan
- Prior art keywords
- slab
- temperature
- titanium alloy
- phase region
- rolling
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Landscapes
- Forging (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
〔産業上の利用分野〕
本発明はチタン合金板の製造方法に関する。
〔従来の技術及びその問題点〕
従来、α+β型チタン合金板を製造する場合、
鋳塊を鍛造又は分塊圧延した広幅大型スラブが使
用されており、このスラブを製造する場合、変形
抵抗の小さいβ域での加工が行われる。このよう
なスラブを更に熱間圧延して得られるチタン合金
板は、一般に組織の均一性や機械的性質(特に伸
び)が著しく劣り、また表面に割れが発生し易い
等の問題を有している。
本発明はこのような従来の問題に鑑み創案され
たもので、均一な組織で伸び等の機械的性質が優
れしかも表面割れの発生しないチタン合金板を製
造し得る方法を提供せんとするものである。
〔発明の構成〕
α+β型チタン合金板製造工程では、鋳塊から
鍛造又は分塊圧延でスラブが作られ、更にこのス
ラブが熱間圧延されるが、このような加工工程を
経た板体が組織の均一性や機械的性質の劣化を生
じるのは、上記したようにβ域で製造されるスラ
ブがその製造段階においてβα+β変態点近傍
温度を徐冷されること等により、その旧β粒界に
粗大粒界α晶がネツトワーク状に析出し、その一
部が熱間圧延やその後の熱処理を経た後も消失す
ることなく引き続き残存することによるものであ
る。従来、このようなスラブの材質や組織面に着
目してスラブ製造段階での加工条件を制御すると
いうような方法は採られていないが、本発明者等
がスラブ製造条件と得られるチタン合金板の組織
及び材質との関係を検討した結果、スラブ製造段
階において鋳塊をα+β2相域の温度において強
加工することにより、熱間圧延後の組織の均一性
や伸び等の機械的性質が著しく改善されることを
見い出した。すなわち、スラブ製造段階で析出し
たネツトワーク状の粗大粒界α晶を消失させるに
は拡散を伴う再結晶を行わせる必要があるが、上
記α+β2相域の温度での強加工により、スラブ
に歪エネルギーが蓄積され、この歪エネルギーに
より、続く熱間圧延での再加熱過程で再結晶が促
進され、これによつて組織の均一化が図られるこ
とが判明したものである。このため本発明は、α
+β型チタン合金鋳塊を、α+β2相域の温度に
おいて全圧下率30%以上で鍛造又は圧延すること
によりスラブとなし、このスラブを再加熱後熱間
圧延するようにしたものである。
また、本発明者等が更に検討したところによれ
ば、熱間圧延をα+β2相域の温度における強圧
下という加工条件で行い、更にかかる熱間圧延前
のスラブ製造工程で上記の如きα+β2相域の温
度での強加工を行うことにより、熱間圧延板の熱
処理後に、より一層均一な組織が得られることが
判明した。すなわち、これは上記のようにしてα
+β2相域で強加工が加えられて歪エネルギーが
蓄積されたスラブが、ネツトワーク状の粗大な粒
界α晶の析出しない温度であるα+β2相域の温
度に加熱されることによつて再結晶をおこし組織
が均一化した後、更にα+β2相域の温度で強加
工の熱間圧延が行われることにより、歪エネルギ
ーが蓄積され、この歪エネルギーで次工程の熱処
理工程において再結晶が促進され、組織が一層均
一化することによるものである。このようなこと
から、本願第2の発明では、α+β型チタン合金
鋳塊を、α+β2相域の温度において全圧下率30
%以上で鍛造又は圧延することによりスラブとな
し、該スラブをα+β2相域の温度に再加熱後、
全圧下率30%以上で熱間圧延すようにしたもので
ある。α+β型チタン合金はα+β2相域の温度
では熱間加工性が低下し、このためα+β温度域
で強加工を加える場合、ネツトワーク状の粒界粗
大α晶の残存するスラブを使用すると、このネツ
トワーク状の粒界粗大α晶を起点として亀甲状の
表面割れが多発するおそれがあるが、上記した発
明では、ネツトワーク状粒界粗大α晶が消失した
スラブを素材として熱間圧延を行うため表面割れ
が防止でき、表面性状の優れた熱間圧延板を製造
することが可能となる。
以下本発明の製造条件を具体的に説明する。
本発明ではまず、α+β型チタン合金鋳塊をβ
変態点−200℃以上、β変態点+100℃以下の温度
に加熱し、途中で強制的に冷却することなく、連
続的にα+β2相域の温度で鍛造あるいは分塊圧
延により全圧下率30%以上の加工を加えて所定寸
法のスラブに成形する。チタン合金鋳塊の加熱は
バツチ炉又は連続炉が用いられる。加熱温度を上
記のように限定したのは次の理由による。すなわ
ちβ変態点−200℃未満の加熱温度ではα+β型
チタン合金の熱間加工性が著しく低下し、表面割
れが発生すると共に熱間変形抵抗が大きくなるた
め圧延が困難となる。一方、加熱温度がβ変態点
+100℃を超えると、チタン合金鋳塊表面の酸化
が著しく、スケールロスの増大及び圧延時の表面
きず発生の原因となる。上記温度域での加工は全
圧下率で30%以上必要であり、30%未満では蓄積
される歪エネルギーが十分でなく続く熱間圧延工
程での組織均一化効果が十分得られない。このよ
うな加工条件で製造されたスラブは、冷却後再加
熱され、熱間圧延されチタン合金板が製造され
る。
次に、本発明の熱間圧延条件は上記加工条件に
より製造したスラブをα+β2相域の温度に加熱
し、α+β2相域の温度で全圧下率30%以上の圧
下を加えて所定寸法の熱間圧延板に圧延する。チ
タン合金スラブの加熱はバツチ炉又は連続炉が用
いられる。加熱温度をα+β2相域の温度と規定
したのは次のような理由による。すなわち、本発
明ではスラブのα+β2相域温度での加熱過程で
スラブ製造過程で蓄えられた材料中の歪エネルギ
ーをもとに再結晶が進み組織が均一化されること
となるが、α+β域よりも高温のβ域温度への加
熱ではβ域温度からの冷却においてβα+β変
態点近傍温度で徐冷されることとなり、旧β粒界
にネツトワーク状の粗大粒界α晶が析出し、本発
明による前記スラブの組織均一化の効果が失われ
るためである。また、α+β2相域の温度での加
工が全圧下率で30%未満では圧延板の熱処理過程
で期待されるような組織の均一化効果が得られな
い。
〔実施例〕
代表的なα+β型チタン合金である第1表に示
す成分系のTi−6%Al−4%V合金鋳塊(直径
550mm)を1050℃に加熱して分塊圧延を行い、120
mm厚さのスラブを作成した。このスラブより切り
出した板厚120mmから45mmまでのスラブを続く熱
間圧延において950〜800℃の温度範囲で36mm厚の
圧延板に仕上げ、圧延まま材とこの圧延後さらに
熱処理(955℃×1.5hr→W.Q.+538℃×6hr→A.
C.)を施した熱処理材(STA材)の各機械的性
質を調べた。この結果を製造条件とともに第2表
に示す。なお、圧延材及び熱処理材の機械的性質
は板厚中心より平行部8.75mmφ,G.L35mmの試験
片をl方向に採取して調査し、また熱処理は125
mml×100mmw×12.5mmtの試験片で行つた。さらに、
α+β型チタン合金の組織はマクロ的な不均一性
が問題となるため、組織の均一性はSTA材につ
いてLZ面におけるα晶の平均粒径(30粒の平均)
を熱処理材の100か所につき測定し、この平均粒
径の標準偏差を各圧延条件で比較することにより
評価した。
[Industrial Field of Application] The present invention relates to a method for manufacturing a titanium alloy plate. [Conventional technology and its problems] Conventionally, when manufacturing an α+β type titanium alloy plate,
Wide, large slabs made by forging or blooming ingots are used, and when manufacturing these slabs, processing is performed in the β region where deformation resistance is low. Titanium alloy plates obtained by further hot rolling such slabs generally have problems such as extremely poor structural uniformity and mechanical properties (particularly elongation), and are prone to cracking on the surface. There is. The present invention was devised in view of these conventional problems, and aims to provide a method for producing a titanium alloy plate with a uniform structure, excellent mechanical properties such as elongation, and no surface cracks. be. [Structure of the Invention] In the α+β type titanium alloy plate manufacturing process, a slab is made from an ingot by forging or blooming rolling, and this slab is further hot rolled. The reason for the deterioration of uniformity and mechanical properties is that as mentioned above, slabs manufactured in the β region are slowly cooled to a temperature near the βα+β transformation point during the manufacturing stage, which causes the deterioration of the former β grain boundaries. This is because coarse grain boundary α crystals precipitate in a network shape, and a part of them continues to remain without disappearing even after hot rolling and subsequent heat treatment. Conventionally, a method of controlling the processing conditions at the slab manufacturing stage by focusing on the material and structure of the slab has not been adopted, but the present inventors and others As a result of examining the relationship between the microstructure and material properties, we found that mechanical properties such as uniformity and elongation of the structure after hot rolling were significantly improved by subjecting the ingot to strong working at temperatures in the α+β2 phase region during the slab manufacturing stage. I found out that it can be done. In other words, in order to eliminate the network-like coarse grain boundary α crystals that precipitate during the slab manufacturing stage, it is necessary to perform recrystallization accompanied by diffusion. It has been found that energy is accumulated and this strain energy promotes recrystallization during the subsequent reheating process during hot rolling, thereby making the structure uniform. Therefore, the present invention provides α
A +β type titanium alloy ingot is forged or rolled at a total reduction rate of 30% or more at a temperature in the α+β2 phase region to form a slab, and this slab is reheated and then hot rolled. Further, according to further studies by the present inventors, hot rolling is carried out under processing conditions of strong reduction at a temperature in the α+β2 phase region, and furthermore, in the slab manufacturing process before such hot rolling, the α+β2 phase region as described above is produced. It has been found that a more uniform structure can be obtained after heat treatment of a hot-rolled plate by performing intense working at a temperature of . That is, this can be done using α as described above.
A slab that has been subjected to heavy working in the +β2 phase region and has accumulated strain energy is recrystallized by being heated to a temperature in the α+β2 phase region where network-like coarse grain boundary α crystals do not precipitate. After the structure is homogenized, strain energy is accumulated by hot rolling at a temperature in the α+β2 phase region, and this strain energy promotes recrystallization in the next heat treatment process. This is due to the organization becoming more uniform. For this reason, in the second invention of the present application, an α+β type titanium alloy ingot is prepared at a total reduction rate of 30 at a temperature in the α+β2 phase region.
% or more to form a slab by forging or rolling, and after reheating the slab to a temperature in the α + β 2 phase region,
Hot rolling is performed at a total reduction rate of 30% or more. The hot workability of α+β type titanium alloys decreases at temperatures in the α+β2 phase region. Therefore, when applying heavy working in the α+β temperature range, if a slab in which network-like grain boundary coarse α crystals remain is used, this net There is a risk that many hexagonal surface cracks may occur starting from the work-like grain boundary coarse α crystals, but in the above invention, hot rolling is performed using a slab in which the network-like grain boundary coarse α crystals have disappeared. It is possible to prevent surface cracking and to produce a hot-rolled plate with excellent surface properties. The manufacturing conditions of the present invention will be specifically explained below. In the present invention, first, α+β type titanium alloy ingot is
The total reduction is 30% or more by heating to a temperature above the transformation point -200℃ and below the β transformation point +100℃, and then continuously forging or blooming at a temperature in the α+β2 phase region without forcibly cooling in the middle. It is then processed to form a slab of specified dimensions. A batch furnace or a continuous furnace is used to heat the titanium alloy ingot. The reason why the heating temperature was limited as described above is as follows. That is, at a heating temperature below the β transformation point -200°C, the hot workability of the α+β type titanium alloy is significantly reduced, surface cracks occur, and hot deformation resistance increases, making rolling difficult. On the other hand, when the heating temperature exceeds the β transformation point +100°C, the surface of the titanium alloy ingot is significantly oxidized, causing increased scale loss and surface flaws during rolling. Processing in the above temperature range requires a total reduction rate of 30% or more, and if it is less than 30%, the accumulated strain energy will not be sufficient and a sufficient effect of homogenizing the structure in the subsequent hot rolling process will not be obtained. The slab manufactured under such processing conditions is cooled, reheated, and hot rolled to manufacture a titanium alloy plate. Next, the hot rolling conditions of the present invention are to heat the slab manufactured under the above processing conditions to a temperature in the α+β2 phase region, apply a reduction with a total reduction rate of 30% or more at a temperature in the α+β2 phase region, and then hot roll the slab to a predetermined size. Roll into rolled plate. A batch furnace or a continuous furnace is used to heat the titanium alloy slab. The reason why the heating temperature was defined as the temperature in the α+β2 phase region is as follows. In other words, in the present invention, during the heating process of the slab at a temperature in the α+β2 phase region, recrystallization progresses based on the strain energy in the material stored in the slab manufacturing process, and the structure becomes uniform. When heating to a high temperature in the β region, cooling from the β region temperature results in gradual cooling to a temperature near the βα+β transformation point, and network-like coarse grain boundary α crystals precipitate at the prior β grain boundaries, which is the result of the present invention. This is because the effect of uniformizing the structure of the slab is lost. Furthermore, if the total reduction ratio of processing at a temperature in the α+β2 phase region is less than 30%, the effect of homogenizing the structure that is expected in the heat treatment process of a rolled plate cannot be obtained. [Example] Ti-6%Al-4%V alloy ingot (diameter
550mm) was heated to 1050℃ and subjected to blooming rolling.
Slabs with a thickness of mm were created. Slabs cut from this slab with thicknesses ranging from 120 mm to 45 mm are then hot-rolled in a temperature range of 950 to 800°C to form rolled plates with a thickness of 36 mm. →WQ+538℃×6hr→A.
C.) The mechanical properties of the heat-treated material (STA material) were investigated. The results are shown in Table 2 together with the manufacturing conditions. The mechanical properties of rolled and heat-treated materials were investigated by taking specimens with a parallel part of 8.75 mmφ and G.L 35 mm from the center of the plate thickness in the l direction.
The test was conducted using a test piece measuring mm l × 100 mm w × 12.5 mm t . moreover,
Macroscopic non-uniformity is a problem in the structure of α+β type titanium alloys, so the uniformity of the structure is the average grain size of α crystals (average of 30 grains) in the LZ plane for STA materials.
was measured at 100 locations on the heat-treated material, and evaluated by comparing the standard deviation of this average grain size under each rolling condition.
【表】【table】
【表】【table】
以上述べた本発明によれば、均一な組織で伸び
等の機械的性質に優れ、しかも表面割れ等のない
チタン合金板を適切に製造することができるとい
う工業上優れた効果がある。
According to the present invention described above, it is possible to appropriately manufacture a titanium alloy plate having a uniform structure, excellent mechanical properties such as elongation, and free from surface cracks, which is an excellent industrial effect.
第1図イ及びロは第2表中No.1材の組織顕微鏡
拡大写真であり、イは圧延まま材、ロは熱処理材
を各示すものである。第2図イ及びロは第2表中
No.6材の組織顕微鏡拡大写真であり、イは圧延ま
ま材、ロは熱処理材を各示すものである。
Figures 1A and 1B are enlarged microscopic photographs of the structure of the No. 1 material in Table 2, with A showing the as-rolled material and B showing the heat-treated material. Figure 2 A and B are in Table 2
This is an enlarged microscopic photograph of the structure of material No. 6, in which A shows the as-rolled material and B shows the heat-treated material.
Claims (1)
温度において全圧下率30%以上で鍛造又は圧延す
ることによりスラブとすることを特徴とするチタ
ン合金板の製造方法。 2 α+β型チタン合金鋳塊を、α+β2相域の
温度において全圧下率30%以上で鍛造又は圧延し
た後、該スラブをα+β2相域の温度に再加熱後、
全圧下率30%以上で熱間圧延することを特徴とす
るチタン合金板の製造方法。 3 熱間圧延板をさらに熱処理することを特徴と
する特許請求の範囲2記載のチタン合金板の製造
方法。[Claims] 1. A method for producing a titanium alloy plate, which comprises forming a slab by forging or rolling an α+β type titanium alloy ingot at a temperature in the α+β2 phase region at a total reduction rate of 30% or more. 2. After forging or rolling an α+β type titanium alloy ingot at a temperature in the α+β2 phase region with a total reduction rate of 30% or more, after reheating the slab to a temperature in the α+β2 phase region,
A method for producing a titanium alloy sheet, characterized by hot rolling at a total reduction rate of 30% or more. 3. The method for producing a titanium alloy plate according to claim 2, characterized in that the hot rolled plate is further heat treated.
Priority Applications (9)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8836184A JPS60234956A (en) | 1984-05-04 | 1984-05-04 | Manufacture of titanium alloy plate |
| US06/725,454 US4581077A (en) | 1984-04-27 | 1985-04-22 | Method of manufacturing rolled titanium alloy sheets |
| CA000479793A CA1257528A (en) | 1984-04-27 | 1985-04-23 | Method of manufacturing rolled titanium alloy sheets |
| FR8506421A FR2565252B1 (en) | 1984-04-27 | 1985-04-26 | PROCESS FOR MANUFACTURING LAMINATED TITANIUM ALLOY SHEETS |
| GB08510702A GB2158373B (en) | 1984-04-27 | 1985-04-26 | Method of manufacturing rolled titanium alloy sheets |
| CA000480302A CA1239077A (en) | 1984-05-04 | 1985-04-29 | Method of producing ti alloy plates |
| GB08511022A GB2162095B (en) | 1984-05-04 | 1985-05-01 | A method of producing ti alloy plates |
| US06/729,299 US4675055A (en) | 1984-05-04 | 1985-05-01 | Method of producing Ti alloy plates |
| FR8506739A FR2563843B1 (en) | 1984-05-04 | 1985-05-03 | METHOD FOR MANUFACTURING TITANIUM ALLOY PLATES |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8836184A JPS60234956A (en) | 1984-05-04 | 1984-05-04 | Manufacture of titanium alloy plate |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60234956A JPS60234956A (en) | 1985-11-21 |
| JPS6320907B2 true JPS6320907B2 (en) | 1988-05-02 |
Family
ID=13940668
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8836184A Granted JPS60234956A (en) | 1984-04-27 | 1984-05-04 | Manufacture of titanium alloy plate |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60234956A (en) |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3481799A (en) * | 1966-07-19 | 1969-12-02 | Titanium Metals Corp | Processing titanium and titanium alloy products |
| JPS5825422A (en) * | 1981-08-05 | 1983-02-15 | Sumitomo Metal Ind Ltd | Manufacture of titanium alloy rolling material having high strength and high ductility |
| JPS5825424A (en) * | 1981-08-05 | 1983-02-15 | Sumitomo Metal Ind Ltd | Manufacture of titanium alloy rolling material having satisfactory texture |
| JPS591660A (en) * | 1982-06-24 | 1984-01-07 | Sumitomo Metal Ind Ltd | Method for working alpha+beta titanium alloy analogous to alpha alloy |
-
1984
- 1984-05-04 JP JP8836184A patent/JPS60234956A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS60234956A (en) | 1985-11-21 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH0686638B2 (en) | High-strength Ti alloy material with excellent workability and method for producing the same | |
| KR20190076749A (en) | Method of processing titanium alloys | |
| KR900006690B1 (en) | Method of producing thin sheet of high si-fe alloy | |
| JPH0613735B2 (en) | Method for producing cube-on-edge oriented silicon steel from strand cast slabs | |
| CA1239077A (en) | Method of producing ti alloy plates | |
| JP2008163361A (en) | Method for producing magnesium alloy thin sheet having uniformly fine crystal grain | |
| US4486242A (en) | Method for producing superplastic aluminum alloys | |
| US4528042A (en) | Method for producing superplastic aluminum alloys | |
| JPS6053727B2 (en) | Method for manufacturing austenitic stainless steel sheets and steel strips | |
| JP2884913B2 (en) | Manufacturing method of α + β type titanium alloy sheet for superplastic working | |
| JPS6320907B2 (en) | ||
| KR20030055286A (en) | Method for producing a cold rolled strip that is cold formed with low degrees of deformation | |
| JPS634908B2 (en) | ||
| JPS634907B2 (en) | ||
| JPS63270448A (en) | Production of alpha type and alpha type titanium alloy plate | |
| JPS63130753A (en) | Manufacture of pure titanium plate reduced in anisotropy of 0.2% yield strength | |
| JPS5925963A (en) | Manufacture of hot rolled ti alloy plate | |
| JPH02310348A (en) | Manufacture of alpha+beta titanium alloy rolled bar and wire having good structure | |
| RU2382114C1 (en) | Manufacturing method of flat profile from zirconium alloys | |
| JPH0665746B2 (en) | Method for manufacturing titanium hot-rolled sheet | |
| JPS61253354A (en) | Manufacture of alpha+beta type titanium alloy sheet | |
| JPH0135915B2 (en) | ||
| JPS62284052A (en) | Method for forging titanium and titanium alloy | |
| KR102239185B1 (en) | Manufacturing method of magnesium alloy plate having excellent formability and magnesium alloy plate using thereof | |
| JPH11124624A (en) | Manufacturing method of austenitic stainless steel plate |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |